Multi-Objective RANS Aerodynamic Optimization of a Hypersonic Intake Ramp at Mach 5

The work describes a systematic optimization strategy for designing hypersonic inlet intakes. A Reynolds-averaged Navier-Stokes database is mined using genetic algorithms to develop ideal designs for a priori defined targets. An intake geometry from the literature is adopted as a baseline. Thus, a s...

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Bibliographic Details
Main Authors: Benini, E. (Author), Bof, D. (Author), De Vanna, F. (Author)
Format: Article
Language:English
Published: MDPI 2022
Subjects:
Online Access:View Fulltext in Publisher